Non-Conventional Propellants and Propulsion System Research and Development at SNECMA Moteurs, 1946-1975

Details Non-Conventional Propellants and Propulsion System Research and Development at SNECMA Moteurs, 1946-1975 Non-Conventional Propellants and Propulsion System Research and Development at SNECMA Moteurs, 1946-1975

Jan 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.304r&link_type=abstract

IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,

Physics

Scientific paper

Since 1944, a wide range of rocket engines and propulsion systems have been develeped by the forebearers of Snecma Moteurs' Large Liquid Rocket Engine branch. Some of them are still in production today and use either "conventional storable" propellants (UDMH and nitrogen tetroxide) or "conventional cryogenic" propellants (liquid oxygen and liquid hydrogen). However a significant amount of research and development has been devoted both to non- conventional propellants and propulsion systems, some of which have seen operational use. Among these, one can quote the following : All these achievements will be described and their historical development outlined in this paper.

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